N433SW

Part: STRINGER — DAMAGED · airframe 42,562 hrs · 37,398 cycles

STRINGER 26L REQUIRES REPLACEMENT BETWEEN FRAME FS364.00 AND APPROX. FS341. (FILED CLOSED) REPLACED DAMAGED SECTION OF STR26L FROM FS364.00 TO SPLICE REPAIR BETWEEN FS333.00 - FS 349.00. SPLICE PERFORMED IN REF TO SRM 53-00-03, FIG 202, SHEET 1 (REPAIR FOR S6764 EXTRUSION). COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH FORM M-337.

Part: RAIL — CORRODED · airframe 42,562 hrs · 37,398 cycles

SEAT TRACK HAS CORROSION BELOW WINDOW 3AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REF TO REO 601R-53-00-775, REV--, DATED 2019-11-21.

Part: RAIL — CORRODED · airframe 42,562 hrs · 37,398 cycles

SEAT TRACK HAS CORROSION DIRECTLY BELOW WINDOW 4AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REF TO REO 601R-53-00-775, REV--, DATED 2019-11-21.

Part: NONE — CORRODED · airframe 42,562 hrs · 37,398 cycles

FRAME 394, FWD LOWER DOUBLER BETWEEN STR 26L AND 27 HAS CORROSION. (FILED CLOSED) REMOVED AND REPLACED SKIN SUPPORT ON FWD SIDE OF FRAME 394.00 BETWEEN STR25L-STR25R IN REF TO SRM 51-42-06 AND REO 601R-53-21-3502, REV--, DATED 2021-09-28. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337

Part: BRACKET — CRACKED · airframe 42,562 hrs · 37,398 cycles

CARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET USING ALTERNATE FASTENERS IN REF TO REO 601R-53-61-7721, REV--, DATED 2021-09-19. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337.

Part: TRACK — GOUGED · airframe 42,562 hrs · 37,398 cycles

CARGO DOOR AFT ROLLER GUIDE TRACK IS GOUGED NEAR THE UPPER STOP. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT ROLLER GUIDE TRACK IN REF TO SRM 51-21-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: VANE — OUT OF LIMITS (RT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

RIGHT INBD FLAP VANE L/E OUTBOARD PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE OTBD PANEL IAW SRM.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

RIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE (CENTER OTBD PANEL) IAW SRM.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

LEFT INBD FLAP VANE CNTER L/E IS CHAFED OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP CENTER VANE PANEL IAW SRM.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

LEFT INBD FLAP VANE OTBD L/E IS CHAFED OUT OF LIMITS. (CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP OTBD L/E VANE PANEL IAW SRM.

Part: FLOOR SUPPORT — OUT OF LIMITS (BS 310-319) · airframe 39,956 hrs · 34,776 cycles

REPLACE RH FLOOR SILL FS 310.00 TO FS 319.70 DUE TO OUT OF LIMITS (C-CHECK) RO: 10/13/2019 R/H FLOOR SILL FS310 TO FS319 REPLACED IAW SRM.

Part: DOOR FRAME — CORRODED (BS 295-310) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR CUT OUT FRAME AT STR 16 1/2 L FROM FS 295.0 TO FS 310.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED INTERCOSTAL ON PAX DOOR CUT OUT FRAME AT STGR 16 1/2 L FROM FS295.00 TO FS310.00 IAW SRM.

Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 39,956 hrs · 34,776 cycles

AFT CARGO DOOR SEAL RETAINER GOUGED UPPER AFT CORNER MARKED (C-CHECK) RO: 10/13/2019 REMOVED CARGO DOOR (UPPER ,AFT ) SEAL RETAINER, AND INSTALLED NEW CARGO DOOR (UPPER ,AFT) SEAL RETAINER IAW SRM.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 39,956 hrs · 34,776 cycles

SERVICE DOOR SILL ANGLE HAS CORROSION (C-CHECK) RO: 10/13/2019 SERVICE DOOR SILL ANGLE IS CORRODED AND REPLACED WITH NEW SILL ANGLE IAW SRM.

Part: DOOR SILL — CORRODED (BS 409) · airframe 39,956 hrs · 34,776 cycles

RH SILL JUST FWD OF SERVICE DOOR CUTOUT AND BACK TO FS 409.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 BLENDED OUT CORROSION ON RH FLOOR SILL FROM FS 310.00 TO FS 319.70 & FROM FS349.00 TO FS409.00 +5 IAW SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR AFT WEB CORRODED AT ACCESS PNL CUTOUTS AND STAIR LANDINGS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR AFT WEB STEP LANDINGS IAW SRM. REMOVED AND REPLACED PAX DOOR AFT WEB IAW SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR FWD WEB CORRODED AT STEP LANDINGS AND ACCESS PNL CUTOUTS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR FWD WEB STEP LANDINGS IAW SRM. REMOVED REPLACED PAX DOOR FWD WEB IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

LEFT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED OUTAND REPAIRED CHAFFING MARKS ON THE LEFT HAND I/B FLAP VANE L/E AT THE 3EA. LOCATION I/B, O/B AND MIDDLE. REPLACED LEFT INBD FLAP (CENTER ) VANE L/E PANEL, AND LEFT INBD FLAP (OTBD ) VANE L/E PANEL IAW REO.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832BR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED CORROSION ON PASSENGER DOOR PANEL 832BR IAW SRM.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832ER HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832ER IAW SRM.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832CR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832CR IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 39,956 hrs · 34,776 cycles

RIGHT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED RIGHT INBD FLAP VANE L/E IN THREE SPOTS ( OUTBD, MIDDLE, INBD). RIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS AND REPLACED. RIGHT INBD FLAP VANE L/E OTBD PANEL IS FOUND TO BE OUT OF LIMITS AND REPLACED. RIGHT INBD FLAP VANE L/E (INBD) PANEL IS WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832AT HAS CORROSION AROUND FASTENER HOLES AND CHAFING DAMAGE ALONG LOWER FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION & CHAFING DAMAGES ON PANEL 832AT AROUND SCREW HOLES IAW SRM.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832GR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832GR, FOUND TO BE OUT OF LIMITS IAW SRM.

Part: PANEL — CORRODED (PAX DOOR) · airframe 39,956 hrs · 34,776 cycles

PAX DOOR PANEL 832EL HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832EL IAW SRM.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 39,931 hrs · 34,749 cycles

CREW REPORTS "GEAR DISAGREE" AFTER TAKEOFF. CREW REPORTED NOSE GEAR WOULD NOT RETRACT AFTER ROTATION. RETURNED TO FIELD. REMOVED AND REPLACED THE NLG STRUT-CENTERED PROXIMITY SENSOR HARNESS ASSY IAW AMM. PERFORMED OPS CHECK OF EXTENSION AND RETRACTION SYSTEM IAW AMM. OPS CHECK GOOD.

Part: SELECTOR VALVE — LEAKING (NLG) · airframe 38,977 hrs · 33,647 cycles

GEAR DISAGREE ON TAKEOFF WHEN TRYING TO RETRACT THE GEAR. BOTH MAINS RETRACTED FULLY BUT THE NOSE GEAR STAYED DOWN. COMPLIED WITH QRH AND ALL GEAR INDICATED DOWN AND 3 GREEN. RETURNED TO FIELD. (FLT#4105) REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. HYD SYS #3 BLEED IAW AMM. PERFORMED FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM IAW AMM. OPS CHECK GOOD. NO LEAKS NOTED. NO GEAR DISAGREE MSG.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 38,970 hrs · 33,642 cycles

FLT#3703, UPON GEAR RETRACTION, NOSE GEAR DID NOT SHOW AN UP INDICATION. GEAR DISAGREE WARNING MESSAGE APPEARED.FOLLOWED QRH PROCEDURE AND GEAR EXTENDED TO DOWN POSITION CORRECTLY. NO GEAR SPEED LIMITS WERE EXCEEDED. INSTALLED NLG SELECTOR VALVE IAW AMM. BLED #3 HYDRAULIC SYSTEM IAW AMM. PERFORMED FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM IAW AMM, OPS CHECK GOOD. NO LEAKS NOTED. NO GEAR DISAGREE MSG.

Part: BRACKET — BENT (NLG) · airframe 38,816 hrs · 33,474 cycles

GEAR DISAGREE ON T/O. NOSE WHEEL DID NOT RETRACT. FOLLOWED QRH. RTF. (FLT#4106) CLOSED REMOVED AND REPLACED NLG OLEO BRACKET AND ADJUSTED PROXIMITY SENSOR. PERFORMED OPS CHECK IAW AMM. OPS CHECK GOOD, SWUNG GEAR MULTIPLE TIMES.

Part: UPLOCK — FAILED (LT MLG) · airframe 38,551 hrs · 33,176 cycles

AS WE PUT DOWN THE LANDING GEAR, WE WOULD GET A MOMENTARY GEAR DISAGREE CAUTION MESSAGE. (FLT# 7413) FO: 10/29/2018. CLOSED REMOVED AND REPLACED LEFT MLG UPLOCK ASSY IAW AMM. LEAK AND OPS CHECKS GOOD.

Part: UNKNOWN — CRACKED (RT WING) · airframe 36,339 hrs · 30,782 cycles

FOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.

Part: UNKNOWN — CRACKED (LT WING) · airframe 36,339 hrs · 30,782 cycles

FOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 36,339 hrs · 30,782 cycles

CARGO FLOOR SUPPORT JUST INSIDE CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED NEW CARGO FLOOR SUPPORT IAW REO.

Part: STRUCTURE — DENTED (LT WING) · airframe 36,339 hrs · 30,782 cycles

WING STATION 139. HAS A DENT 3/4 INCH WIDE AND .010 INCH DEEP. HAND FORMED THE DENT BACK TO ORIGINAL CONTOUR IAW REO. CHECKED GOOD..

Part: STRUCTURE — DENTED (LT WING) · airframe 36,339 hrs · 30,782 cycles

LEFT WING LEADING EDGE LWS 185. HAD A SMALL DENT THAT MEASURES .019 INCH IN DEPTH, X .75 INCH IN LENGTH, AND .5 INCH IN WIDTH. COMPLIED WITH DRESS BACK REPAIR TO DENT ON THE LH WING LEADING EDGE IAW REO. LEAK CHECKED GOOD.

Part: SKIN — DENTED (RT WING) · airframe 36,339 hrs · 30,782 cycles

RT WING LEADING EDGE WING STATION 166. HAD A SMALL DENT .009 INCH DEEP X 3/4 INCH WIDE AND 1/2 INCH LONG. HAND DRESSED THE SKIN BACK TO ORIGINAL CONTOUR IAW REO.CHECKED GOOD.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 35,503 hrs · 29,843 cycles

PILOT REPORTED NOSE GEAR WOULD NOT RETRACT WITH GEAR DISAGREE. REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. SWUNG GEAR, OPS CHECKED GOOD.

Part: STRUT — OVERSERVICED (NLG) · airframe 33,329 hrs · 27,518 cycles

NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. FOUND NOSE STRUT OVER SERVICED CORRECTED, OPS CHECKS GOOD, GEAR SWING ACCOMPLISHED.

Part: BRACKET — BENT (NLG) · airframe 31,520 hrs · 25,765 cycles

ON DEPARTURE, NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. MAIN GEAR EXTENDED NORMALLY. DUE TO IMPROPER PLACEMENT OF TOW STRAP, R & R BENT AND MISALIGNED NLG CENTERED PROX SENSOR BRACKET IAW AMM, PN: 16215-105.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,811 hrs · 25,062 cycles

LEFT MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LIGHT — BURNED OUT (EXTERIOR) · airframe 30,587 hrs · 24,850 cycles

EXTERIOR EMERGENCY LIGHT NR 7 IS BURNED OUT. R & R EXTERIOR EMERGENCY LIGHT IAW AMM.

Part: ACTUATOR — FAILED (YAW DAMPER) · airframe 30,393 hrs · 24,671 cycles

YAW DAMPER NR 2 KEEPS DISCONNECTING AND WHEN ENGAGED CAUSES UNCOMMANDED RUDDER MOVEMENT. R & R YAW DAMPER NR 2 LINEAR ACTUATOR IAW AMM, PN ON/OFF: 622-9968-001, SN ON: 2497, SN OFF: 2561.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,208 hrs · 24,487 cycles

EMERGENCY LIGHT NEXT TO MAIN CABIN DOOR IS BURNED OUT. FLT 4699 RELAMPED.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 29,993 hrs · 24,262 cycles

AIRCRAFT INITIATED A SEVERE CLIMB TO CAPTURE GLIDE SLOPE, DISCONNECTED THE AUTO PILOT, GOT THE AIRCRAFT STABLE & RESUMED THE APPROACH. WHEN THE AUTO PILOT WAS RECONNECTED, AT APPROXIMATELY 3500 ', THE FLIGHT DIRECTOR COMMANDED A 15 DEGREE NOSE DOWN PITCH. DISCONNECTED THE AUTO PILOT AGAIN & HAND FLEW THE REST OF THE APPROACH. FLT 7368 REPLACED FCC 1 PN ON OFF 622-9815-904, SN ON FXCW & SN OFF 1755.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,692 hrs · 23,978 cycles

CABIN FLOOR SUPPORT BEAM FS 349.00 AT PAX DOOR HAS CORROSION ON UNDERSIDE & CORRODED FASTENERS. C-CHECK REPAIRED CABIN FLOOR SUPPORT BEAM AT FS 349 LBL 40.00 IAW STS EA.

Part: STIFFENER — CHAFED (WING) · airframe 29,692 hrs · 23,978 cycles

INTERNAL LT SIDE OF CTR WING FUEL TANK, FUEL PANEL 510BB. FUEL TUBE ASSEMBLY IN FWD PORTION OF TANK, CHECK VLV IS CHAFING ON THE STIFFENER. C-CHECK BLENDED CHAFED AREA ON STRINGER 23 JUST OTBD OF WS 29.4 IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,692 hrs · 23,978 cycles

AFT PRESSURE BULKHEAD, AFT SIDE, FRAME JUST AFT OF BULKHEAD HAS 2 EA CRACKED "L" ANGLES, 1 AT LT SIDE, 1 AT RT SIDE. C-CHECK R & R 2 EA "L" ANGLES AT FS 625 STRINGER 14 IAW SRM & REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,692 hrs · 23,978 cycles

RT AILERON UPPER LE SKIN IS CHAFED. C-CHECK REPLACED RT AILERON UPPER LE SKIN PN 601R13031-166 IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,692 hrs · 23,978 cycles

RT AILERON LOWER LE SKIN CHAFED INBD OF CTR HINGES. C-CHECK BLENDED, EVALUATED, & RESTORED CHAFED AREA OF RT AILERON LOWER LE SKIN, INBD OF CTR HINGES. R & R 2 RIVETS IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,692 hrs · 23,978 cycles

RT INBD FLAP VANE LE CHAFED AT WS139.924. C-CHECK BLENDED RT INBD FLAP VANE LE CHAFE AT WS 139.924 IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 29,692 hrs · 23,978 cycles

LT AILERON UPPER LE SKIN CHAFED SEVERAL AREAS FROM OTBD TO INBD ENDS. C-CHECK BLENDED CHAFED AREAS ON LT AILERON UPPER LE SKIN IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,692 hrs · 23,978 cycles

RT INBD FLAP VANE LE CHAFED AT WS56.30. C-CHECK BLENDED RT INBD FLAP VANE LE CHAFE AT WS 56.30 IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,692 hrs · 23,978 cycles

RT INBD FLAP VANE LE CHAFED AT WS104.099. C-CHECK BLENDED RT INBD FLAP VANE LE CHAFE AT WS 104.099 IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 29,692 hrs · 23,978 cycles

LT AILERON LOWER LE SKIN CHAFED INBD OF CTR HINGES. C-CHECK BLENDED CHAFED AREA ON LT AILERON LOWER LE SKIN INBD OF CTR HINGES. IAW REO.

Part: ACCESS PANEL — CHAFED (AILERON) · airframe 29,692 hrs · 23,978 cycles

AILERON HINGE ACCESS PANEL 699AB HAS CHAFE MARK. C-CHECK BLENDED, EVALUATED, & FINISHED CHAFED AREA ON AILERON HINGE ACCESS PANEL 699AB IAW REO & SRM.

Part: ACCESS PANEL — CHAFED (AILERON) · airframe 29,692 hrs · 23,978 cycles

AILERON HINGE ACCESS PANEL 699BB HAS CHAFE MARK. C-CHECK BLENDED, EVALUATED, & RESTORED FINISH TO CHAFED AREA ON AILERON HINGE ACCESS PANEL 699BB IAW REO & SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,828 hrs · 23,137 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMPS.

Part: SIGN — LOOSE (CABIN) · airframe 28,378 hrs · 22,703 cycles

RIGHT EMERGENCY EXIT SIGN ON RIGHT SIDE LOOSE. (SERVICE) RESCURED RIGHT EMERGENCY EXIT SIGN, OPS CHECK GOOD.

Part: FLAP — DIRTY (WING) · airframe 28,332 hrs · 22,658 cycles

AIRCRAFT ROLLS HARD TO RIGHT WHEN FLAPS ARE PAST 42 DEGREES. TRIM PAST HALF WAY MARK, LEFT WING DOWN REQUIRED TO KEEP AIRCRAFT BALANCED. (FLT 4521) CLEANED EXTREMELY DIRTY FLAP SURFACES.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 28,332 hrs · 22,658 cycles

STARTED APU BUT HAD NO LIGHT OFF, SHUT DOWN APU, STARTED APU SECOND TIME AND IT STARTED NORMALLY. FOLLOWING APU START HOWEVER, HAD FUEL SMELL ENTER COCKPIT. (FLT7368) INSPECTED APU, NO LEAKS NOTED. COMPLIED WITH APU START/STOP. NO SMELL NOTED AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,103 hrs · 22,422 cycles

OVERHEAD EMERGENCY LIGHTS TURN ON THEN FADE OFF. (FLT 4842) SET EMERGENCY LIGHTS IN ARM POSITION TO ALLOW BATTERY PACKS TO CHARGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,616 hrs · 21,937 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4466) RELAMPED EMERGENCY LIGHT.

Part: DOOR — CRACKED (TRU BAY) · airframe 28,072 hrs · 22,391 cycles

CRACK BELOW AFT LATCH OF LEFT TRU BAY DOOR. (SERVICE) INSTALLED NEW LEFT TRU DOOR, DOOR LANDING AND APPLIED SEALANT IAW SRM AND AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,343 hrs · 21,681 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,191 hrs · 21,531 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4735) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,810 hrs · 21,160 cycles

FLT 4838, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,734 hrs · 21,084 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4521) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,612 hrs · 20,972 cycles

NR 2 MIDDLE EMERGENCY LIGHT ON LEFT WING IS OUT. (FLT 4835) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,585 hrs · 20,944 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4758) RELAMPED EMERGENCY LIGHT,

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,287 hrs · 20,679 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4561) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,287 hrs · 20,679 cycles

NR 2 OVERHEAD EMERGENCY EXIT SIGN IS INOP. (FLT 7806) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,220 hrs · 20,615 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4473) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,139 hrs · 20,547 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 7771) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,139 hrs · 20,547 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: POST — CRACKED (FUSELAGE) · airframe 26,125 hrs · 20,536 cycles

LEFT AND RIGHT FS 409+128 VERTICAL POSTS ARE CRACKED. (C-CHECK) REPLACED LEFT AND RIGHT FS 409+128 VERTICAL POSTS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,244 hrs · 21,581 cycles

LEFT SIDE FS 559.0 PRESSURE BULKHEAD IS CRACKED. (C-CHECK) REPAIRED PER REO.

Part: VANE — CHAFED (TE FLAP) · airframe 27,244 hrs · 21,581 cycles

RIGHT OUTBOARD FLAP VANE ON INBOARD FLAP CHAFED. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 REO.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 27,244 hrs · 21,581 cycles

CARGO BAY FLOOR EDGE MEMBER ON THE INBOARD AND OUTBOARD SIDE OF LBL 27 IS CORRODED. (C-CHECK) REPAIRED IAW CRJ200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,857 hrs · 20,295 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4808) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,806 hrs · 20,244 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4824) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,729 hrs · 20,166 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4613) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,652 hrs · 20,091 cycles

NR 5 EXTERIOR AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4474) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,550 hrs · 19,996 cycles

LEFT WING CENTER EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4750) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,476 hrs · 19,928 cycles

SECOND TO LAST CEILING EMERGENCY LIGHT IS BURNED OUT. (FLT 4609) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,417 hrs · 19,876 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4814) RELAMPED EMERGENCY LIGHT.

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 25,204 hrs · 19,674 cycles

(FLT 4779) RIGHT MAIN LANDING GEAR DID NOT EXTEND NORMALLY. CYCLED GEAR HANDLE AND GEAR CAME DOWN AND LOCKED. REPLACED RIGHT SIDESTAY ACTUATOR, RIGHT MLG UPLOCK, MLG SELECTOR VALVE, RUN AROUND BYPASS VALVE, MLG PRIORITY VALVE AND RESTRICTOR VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,923 hrs · 19,427 cycles

LEFT OVERWING FORWARD EMERGENCY LIGHT IS OUT. (FLT 4500) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,923 hrs · 19,427 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4800) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,967 hrs · 18,634 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4848) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,860 hrs · 18,547 cycles

EMERGENCY LIGHTS WILL NOT STAY ON. (FLT 4682) REPLACED ALL 4 ELBP'S.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 22,886 hrs · 17,675 cycles

LEFT ENGINE YOKE LINK BUSHING PITTED. (ENG CHANGE) REPLACED BUSHING PER AMM.

Part: PCU — MALFUNCTIONED (ELEVATOR) · airframe 22,829 hrs · 17,601 cycles

WITH SYSTEM NR 3 HYDRAULICS ON, RIGHT ELEVATOR FULLY DEFLECTS DOWN. (FLT 4529) REPLACED RIGHT ELEVATOR NR 3 PCU.

Part: DOOR — MALFUNCTIONED (CABIN DOOR) · airframe 22,413 hrs · 17,249 cycles

MAIN CABIN DOOR HARD TO CLOSE. (FLT 4779) OPERATIONAL CHECK NORMAL.

Part: WEB — CRACKED (BS 280) · airframe 22,047 hrs · 16,950 cycles

C-CHECK, FS 280 WEB CRACKED. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (BS 559) · airframe 22,047 hrs · 16,950 cycles

C-CHECK, FS 559 PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 21,120 hrs · 16,193 cycles

GEAR DISAGREE DISPLAYED. (FLT 4869) REPLACED NLG SELECTOR VALVE.

Part: STRUT — DISCHARGED (NLG) · airframe 19,891 hrs · 15,233 cycles

FLT 4636 - NOSE GEAR DISAGREE AFTER TAKEOFF. SERVICED NOSE GEAR PER AMM.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 19,572 hrs · 14,994 cycles

FLT 4865 - 'GEAR DISAGREE' FROM NOSE GEAR. REPLACED THE PRIORITY VALVE FOR THE NOSE LANDING GEAR.

Part: ACM — SMOKE (RIGHT) · airframe 18,210 hrs · 13,925 cycles

FLT 3743 - ON TAXI OUT, CABIN FILLED WITH SMOKE. REPLACED RIGHT PACK AIR CYCLE MACHINE WITH SERVICEABLE UNIT AS REQUIRED. OPS CHECK GOOD IAW CRJ AMM 21-51-10.

Part: SWITCH — STICKS (FIRE BOTTLE) · airframe 18,400 hrs · 14,064 cycles

NR 2 ENGINE FIRE BOTTLE DISCHARGE SWITCH LIGHT STICKS CLOSED. (FOUND AT C-CHECK) REPLACED INNER SWITCH CONTACTS PER AMM 26-21-01-000-802.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 18,400 hrs · 14,064 cycles

EMERGENCY LIGHT STRIP IN CABIN IS INOP. (FOUND AT C-CHECK) REPAIRED LIGHTING WIRING PER ESPM 20-17-00 AND WDM 33-51-00.

Part: TUBE — DEFORMED (EXTINGUISHER) · airframe 18,400 hrs · 14,064 cycles

BAGGAGE FIRE EXTINGUISHER TUBE IS KINKED. (FOUND AT C-CHECK) REPLACED KINKED DISCHARGER TUBE PER CRJ200 AMM 26-25-07-400-801.

Part: SEAL — BINDING (SERVICE DOOR) · airframe 17,604 hrs · 13,449 cycles

FLT 3906 - GALLEY SERVICE DOOR IS EXTREMELY HARD TO OPEN. REPLACED GALLEY SERVICE DOOR SEAL IAW MM 52-41-02.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 17,649 hrs · 13,484 cycles

FLT 3911 - EMERGENCY LIGHT COVER ON LEFT SIDE OF ENTRANCE FELL OFF. REPLACED LIGHTED SIGN ASSEMBLY IAW 33-00-00. OPS CHECK GOOD.

Part: TORQUE LINK — DISCONNECTED (MLG) · airframe 16,034 hrs · 12,231 cycles

RECEIVED A GEAR DISAGREE WARNING AND A NOSE DOOR OPEN WARNING WHEN SELECTING GEAR UP. RETURNED TO DFW. FOUND TORQUE LINKS DISCONNECTED AND NOSE TIRES SHOWING CHORD. REMOVED AND REPLACED BOTH NOSE WHEEL ASSYS IAW AMM 32-42-01, PN 5010598, SN OFF NOV02-4502 PN 5010598, SN OFF: MAY03-0142.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,164 hrs · 10,868 cycles

NUMEROUS CRACKS LOWER INBOARD CORNERS OF PILOT/CO-PILOT FORWARD WINDOWS. REPLACED BOTH WINDSHIELDS IAW 56-11-01 AND RII 56-220-1000. OPERATIONAL/PRESSURE CHECKS GOOD, SN OFF: 01115H6386 AND SN OFF: 01115H6374.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,883 hrs · 10,667 cycles

FS280 LBL9 INBD CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP P/N 601R31113-57 PO 64963 PER CRJ 200 SRM 51-42-06; 51-42-21 AND 51-40-11 PG 4 AND 5 AT FS 280 LBL9.

Part: ANGLE — CRACKED (WING) · airframe 13,883 hrs · 10,667 cycles

RT SIDE BATT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REO 601R-57-51-046-6 & -8 IAW REO 601R-57-51-046 NOTES 5-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,883 hrs · 10,667 cycles

FS 280 RBL9 INBD CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601R31113-58 AT FS 280; RBL 9.0; IB SIDE AS PER CRJ 200 SRM 51-42-06 PGS 1-6 AND 51-42-21 PGS 1-21.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 13,883 hrs · 10,667 cycles

PAX DOOR CRACK IN STAIR SUPPORT STRUCTURE UNDER THE AFT SIDE HOLD DOWN BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ANGLE ON PAX DOOR; AFT SIDE AT HOLD DOWN BRACKET LOCATION IAW CRJ 200 REO 601R-52-11-702.

Part: BEAM — CRACKED (FUSELAGE) · airframe 13,883 hrs · 10,667 cycles

FS 280 BEAM CRACKED ON AFT SIDE APPROXIMATELY RBL 12 AT FLOOR SUPPORT VERTICAL STIFFENER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PART IAW CRJ 200 REO 601R-53-11-171(C) AND REO 601R-53-11-1042.

Part: TRANSMITTER — INOPERATIVE (RUDDER) · airframe 12,319 hrs · 9,477 cycles

NO RUDDER DEFLECTION INDICATION ON FLIGHT CONTROL SYNOPTIC. REPLACED THE RUDDER POSITION TRANSMITTER PER MM 27-24-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 12,268 hrs · 9,441 cycles

SPOILERONS FAULT, OUTBOARD GND SPOILER FAULT STATUS MESSAGES EN ROUTE. REPLACED SECU NR 1 IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — STICKING (COCKPIT) · airframe 11,373 hrs · 8,757 cycles

FO'S TRIM SWITCH STICKING. REPLACED FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (LT SPOILER) · airframe 10,922 hrs · 8,405 cycles

AFTER TAKEOFF IN YYC, HAD A SPOILERON FAULT STATUS MESSAGE WHICH STAYED ON THE ENTIRE FLIGHT. REPLACED LEFT SECU IAW 27-61-05. OPS CHECK GOOD.

Part: TRIM SWITCH — STICKING (COCKPIT) · airframe 10,460 hrs · 8,044 cycles

CAPTAINS TRIM SWITCH STICKY. REPLACED CAPTAINS TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 9,725 hrs · 7,473 cycles

AFT SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. P/N 2013-1A, S/N OFF 42053.

Part: TRIM PANEL — DEFECTIVE (COCKPIT) · airframe 9,228 hrs · 7,087 cycles

RUDDER TRIM WON’T GO NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,515 hrs · 7,311 cycles

LEFT INBOARD FS 280 BRACKET IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE PER CRJ 200 SRM 51-42-06 AND 51-42-20.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,515 hrs · 7,311 cycles

RIGHT SIDE FS 621.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2 ANGLE, -6 ANGLE, -6 STRAP AND -302 ANGLE PER CRJ 200 REO 601R35-61-117.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,515 hrs · 7,311 cycles

FLOORBEAM AT STA 280 RBL 9.1 CRACKED ON INBOARD AND OUTBOARD SIDES OF FLOORBEAM WEB, AND AT LEFT OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLES IAW CRJ 200 SRM 51-42-06 FIG 8, 51-42-21 FIG 10.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 8,642 hrs · 6,629 cycles

SMOKE CARGO ILLUMINATED ON GROUND. REMOVED AND REPLACED NR 2 SMOKE DETECTOR IAW 26-15-01, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (RUDDER TRIM) · airframe 7,691 hrs · 5,879 cycles

RUDDER TRIM WILL NOT RE-CENTER; ONLY MOVES NR, WILL NOT RETURN NL. CLEANED CONNECTOR AND PINS. OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,895 hrs · 5,267 cycles

OVERHEAD EMERGENCY LIGHT IN AFT CABIN INOP. REMOVED AND REPLACED EMERGENCY LAMP WITH A NEW LAMP IAW 33-00-00. OPS CHECK GOOD. P/N: 1317.

Part: ACTUATOR — MALFUNCTIONED (PITCH FEEL) · airframe 6,201 hrs · 4,747 cycles

FLIGHT CONTROL MOVEMENT IS MUCH HEAVIER THAN NORMAL (PITCH). REPLACED CO-PILOT'S PITCH FEEL LINEAR ACTUATOR IAW CRJ MM 27-31-23. OPS CHECKS GOOD.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 5,954 hrs · 4,573 cycles

DURING STALL TEST, SHAKER DOES NOT ACTIVATE. REPAIRED BROKEN WIRE IAW CL 600 WDM 20-00-00. OPS CHECK GOOD.

Part: ECU — FAULTY (NR 1) · airframe 5,341 hrs · 4,112 cycles

OUTBOARD GROUND SPOILER STATUS MESSAGE. REPLACED SECU NR 1. OPS CHECKS GOOD IAW CRJ MM 27-61-05.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 4,767 hrs · 3,657 cycles

ON TAXI IN RETRACTING FLAPS FROM 30 DEGREES TO 20 DEGREES, RECEIVED FLAPS FAIL MESSAGE AND FLAPS REMAINED AT 30 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW MM 27-51-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,783 hrs · 3,670 cycles

FS 621.00 LBL 36 FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE AREA IAW CRJ REO 601R-53-61-117 REV A & RII53-401.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,783 hrs · 3,670 cycles

FLOORBEAM ATTACH ANGLES AT FS 280 LBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 4,783 hrs · 3,670 cycles

PILOT STICK SHAKER INOP. BROKEN WIRE. DISCOVERED DURING C-CHECK. INSTALLED NEW TERMINAL ENDS ON PILOT SIDE STICK SHAKER WIRES IAW AWM CHAPTER 27-35-00. OPS TESTED SPS (PRE-FLIGHT TEST) IAW AMM TASK 27-35-01-710-801. TEST SERVICEABLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,783 hrs · 3,670 cycles

CABLE FAIRLEAD INTERCOSTAL AT FS 484 IS CRACKED AT RBL 36. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R53-41-059 REV A (RII53-401).

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,783 hrs · 3,670 cycles

FLOORBEAM ATTACH ANGLES AT FS 280 RBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401.

Part: CONTROL UNIT — MALFUNCTIONED (NR 1 SPOILER) · airframe 4,330 hrs · 3,328 cycles

SPOILERONS FAULT STATUS MESSAGE UNABLE TO CLEAR. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM 27-60-01. OPS AND LEAK CHECK GOOD. UPDATE 3/27/03: SPOILERONS FAULT MESSAGE DISPLAYED NON ED-2. REMOVED AND REPLACED NR 1 SECU. OPS CHECK GOOD IAW CRJ MM 27-60-00.

Part: SPRING — OBSTRUCTED (CABIN DOOR) · airframe 2,947 hrs · 2,271 cycles

MAIN CABIN DOOR IS EXTREMELY DIFFICULT TO OPEN. INSPECTED DOOR MECHANISM AND FOUND INSIDE LATCH STOW SPRING DIFFICULT TO COMPRESS. CLEARED DEBRIS FROM SPRING. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 2,748 hrs · 2,113 cycles

STAB CHANNEL NR 1 INOP. REMOVED & REPLACED STAB TRIM ACTUATOR & MOTOR CONTROL UNIT IAW 27-40-00, 27-42-01, 27-42-05. OPS CHECKS GOOD.

Part: COMPUTER — FAILED (COCKPIT) · airframe 1,930 hrs · 1,481 cycles

COPILOT'S PFD FAILED WITH ASSOCIATED MAG FAIL FLAG AND FLIGHT DIRECTOR FAILED FLAG. NO EFIS COMP MON OR COMPARITOR MESSAGES. REMOVED AND REPLACED NR 2 AHC89E. OPS CHECK GOOD. RELEASED FOR CAT II OPERATIONS.

Part: CONTROL UNIT — FAILED (SPOILER) · airframe 208 hrs · 149 cycles

ON TAXI OUT FLT SPLRS AND SPOILERON CAUTION LIGHT ON. INSTALLED SERVICEABLE SECU AT LEFT POSITION. PERFORMED OPS CHECK OF SPOILER SYSTEM. OPS CHECK GOOD. S/N OFF: 1329.